Gas turbine engine

Power plants – Combustion products used as motive fluid – Multiple fluid-operated motors

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60 3936, 60 3975, 60744, 415114, F02C 716

Patent

active

050037668

ABSTRACT:
A gas turbine engine that can operate at a very high efficiency over a wide range of load conditions. In one important feature of the invention, combustion gases are discharged along two paths, one with constant energy and the other with energy that varies in accordance with the engine load. The constant energy discharge drives a turbine that, in turn, operates a compressor for the engine at a constant, high efficiency. Alternatively, the compressor is driven at a speed that varies inversely with the engine load such that the engine operates at a high efficiency for all loads. In another, independent feature of the invention, the combustion occurs at a stoichiometric ratio of fuel and air, with the turbine blades being protected from the vastly increased combustion gas temperatures by an internal array of passageways through which cooling liquid, e.g., liquid fuel, and air are channeled. The fuel and air mix together to form a rich, turbulent pre-mix for ejection directly into the surrounding combustion chamber. This configuration can also be utilized to inject steam into the combustion chamber, to provide a Rankine cycle, with internal cogeneration. In yet another independent aspect of the invention, the compressor that supplies compressed air to the combustion chamber includes two counter-rotating radial impellers, with the second impeller further functioning as a diffuser for the first impeller.

REFERENCES:
patent: 1977958 (1934-10-01), Van Rijswijk
patent: 2095991 (1937-10-01), Lysholm
patent: 2365616 (1944-12-01), Zweifel
patent: 2414551 (1947-01-01), Pavlecka et al.
patent: 2416389 (1947-02-01), Heppner
patent: 2575682 (1951-11-01), Price
patent: 2595505 (1952-05-01), Bachle
patent: 2603063 (1954-11-01), Ray
patent: 2647368 (1954-08-01), Triebbnigg et al.
patent: 2705865 (1955-04-01), Mann
patent: 2853227 (1958-09-01), Beardsley
patent: 2924937 (1960-02-01), Leibach
patent: 3113430 (1963-12-01), Beal et al.
patent: 3161018 (1964-12-01), Sandre
patent: 3238716 (1966-03-01), Sandre
patent: 3446481 (1969-05-01), Kydd
patent: 3472487 (1969-10-01), Moellmann
patent: 3528250 (1970-09-01), Johnson
patent: 3533712 (1970-10-01), Kercher
patent: 3548597 (1970-12-01), Etessam
patent: 3600890 (1971-08-01), White
patent: 3635029 (1972-01-01), Menioux
patent: 3806275 (1974-04-01), Aspinwall
patent: 3856433 (1974-12-01), Grondahl et al.
patent: 3978663 (1976-09-01), Mandrin et al.
patent: 4010608 (1977-03-01), Simmons
patent: 4041699 (1977-08-01), Schelp
patent: 4054030 (1977-10-01), Pederson
patent: 4118145 (1978-10-01), Stahl
patent: 4175384 (1979-11-01), Wagenknecht et al.
patent: 4190398 (1980-02-01), Corsmeier et al.
patent: 4242045 (1980-12-01), Grondahl et al.
patent: 4338780 (1982-07-01), Sakamoto et al.
patent: 4376375 (1983-03-01), Boudigues

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Gas turbine engine does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Gas turbine engine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Gas turbine engine will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-319974

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.